US2010028160A1PendingUtilityA1

Compressor blade leading edge shim and related method

48
Assignee: GEN ELECTRICPriority: Jul 31, 2008Filed: Jul 31, 2008Published: Feb 4, 2010
Est. expiryJul 31, 2028(~2.1 yrs left)· nominal 20-yr term from priority
F04D 29/023F05D 2260/95Y10T29/49337F05D 2230/23F01D 5/005F05D 2230/80F04D 29/324F05D 2300/2284F05D 2240/303F01D 5/28
48
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Claims

Abstract

A method of improving an erosion resistance at the leading edge of a compressor blade includes: a) cleaning a leading edge portion of the compressor blade airfoil; and b) attaching one or more erosion or corrosion-resistant shims to the leading edge portion.

Claims

exact text as granted — not AI-modified
1 . A compressor blade comprising an airfoil portion and a mounting portion; the airfoil portion having leading and trailing edges, the leading edge having an erosion-resistant shim attached thereto. 
   
   
       2 . The compressor blade of  claim 1  wherein said shim is comprised of a material selected from a group comprising TiN, Ti/TiN, TiN/CrN, NiCrWC. 
   
   
       3 . The compressor blade of  claim 1  wherein the shim is composed at least in part of a composition selected from a group comprising Cr, Al or Ti-rich materials. 
   
   
       4 . The compressor blade of  claim 1  wherein the shim is comprised of a metal coated with an erosion or corrosion resistant material. 
   
   
       5 . The compressor blade of  claim 1  wherein said shim is attached by welding, brazing or soldering. 
   
   
       6 . The compressor blade of  claim 1  wherein said shim is attached by adhesive. 
   
   
       7 . The compressor blade of  claim 1  wherein said shim comprises plural shim segments. 
   
   
       8 . The compressor blade of  claim 1  wherein said shim is between about 1 and about 25 mils thick. 
   
   
       9 . The compressor blade of  claim 1  wherein said shim is made of a polymeric material. 
   
   
       10 . The compressor blade of  claim 9  wherein said polymeric material comprises polypropylene. 
   
   
       11 . A method of improving an erosion/corrosion resistance at the leading edge portion of a compressor blade airfoil comprising:
 a) preparing the leading edge portion of the compressor blade airfoil; and   b) attaching one or more shims to said leading edge portion.   
   
   
       12 . The method of  claim 11  wherein step (a) is carried out by milling, shot-peening, grit blasting, vibratory finishing or combinations thereof. 
   
   
       13 . The method of  claim 11  wherein said shim said shim is comprised of a material selected from a group comprising TiN, Ti/TiN, TiN/CrN, NiCrWC. 
   
   
       14 . The method of  claim 11  wherein the shim is composed at least in part of a composition selected from a Cr, Al or Ti-rich material. 
   
   
       15 . The method of  claim 11  wherein the shim is comprised of a metal coated with an erosion or corrosion resistant material. 
   
   
       16 . The method of  claim 11  wherein said shim is attached by welding, brazing or soldering. 
   
   
       18 . The method of  claim 11  wherein said shim is attached by adhesive. 
   
   
       19 . The method of  claim 11  wherein said shim is made of a polyurethane tape. 
   
   
       20 . The method of  claim 11  wherein said shim is made of a polymeric material.

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